SGS 2-33 Schweizer   


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General Details
Manufacturer: Schweizer
Plane Name:

SGS 2-33

Classified as: Unclassified
Country Of Origin: U S A
Designer: Ernest Schweizer
No. of Seats 2
No. Built 579
   
Performance:
L/DMax: 23 72 kph / 39 kt / 45 mph
   
MinSink: 0.85 m/s / 2.8 fps / 1.66 kt
   


 

Specifications:
Span Area Empty Weight Payload Gross Weight Wing Load Water Ballast
m ft sq.m sq.ft kg lb. kg lb. kg lb. kg
/sq.m
lb.
/sq.ft
kg lb.
15.54 51 20.39 219.5 272 600 200 440 472 1040 23.15 4.73 0 0
Aspect ratio: 18
Airfoil: NACA 4301 2A
Structure: steel tube/ aluminum skin/ Ceconite fabric
Engine:

Comment:
The 2-33 was designed to succeed the 2-22 as something a little plusher and better performing, therby making it easier to attract new students into soaring. The prototype 2-33 first flew in 1965 and volume production began in 1967. For the best part of the following 20 years, 2-33メs were mainstays in U.S. glider pilot training. It has an all-metal wing structure and steel tube fuselage with moving tail surfaces covered in Ceconite fabric. The spoilers are aerodynamically balanced. The A model, introduced in 1968, has a larger rudder. Subsequent minor offered as an FAA-approved homebuilders kit. The U.S. Air Force Academy operates 13 as the TG-4A. ATC


           

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